WEKO3
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超音速機用推進システムにおける混合流解析
https://jaxa.repo.nii.ac.jp/records/36780
https://jaxa.repo.nii.ac.jp/records/3678045d4f02c-0fed-43f1-868a-6b0d309b083d
名前 / ファイル | ライセンス | アクション |
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nalsp0030012.pdf (285.2 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 超音速機用推進システムにおける混合流解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ラムジェット機関 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 混合流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ミキサエジェクタノズル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 騒音抑制 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 排気ジェット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気取入口 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | モード切換 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流混合 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子形成 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 模型試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推進システム | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ramjet engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersupersonic transport | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic mixing flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mixer ejector nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | noise control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | exhaust jet | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | air intake inlet | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mode changing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent mixing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent flow model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid generation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | model test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propulsion system | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Analysis of mixing flows for the hypersupersonic transport propulsion system | |||||
著者 |
大石, 勉
× 大石, 勉× 平井, 健二× 児玉, 秀和× 宮城, 裕幸× 山本, 誠× 田村, 敦宏× 菊地, 一雄× 野崎, 理× Oishi, Tsutomu× Hirai, Kenji× Kodama, Hidekazu× Miyagi, Hiroyuki× Yamamoto, Makoto× Tamura, Atsuhiro× Kikuchi, Kazuo× Nozaki, Osamu |
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著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
東京理科大学 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Science University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 30, p. 65-68, 発行日 1996-01 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 7-9 Jun. 1995 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 超音速機用推進システムにはさまざな混合を伴う流れがある。例えば、離陸時の騒音レベルを下げるためのミキサエジェクタノズル内における排気ジェットと取入空気との混合、燃焼モード切り換え時における前部混合部でのラム側空気とターボ側空気の混合などである。本推進システムの研究開発においては、このような混合流の特性を予測することがシステム設計や性能改善にとって重要である。ここでは、前述のミキサエジェクタノズルおよび前部混合部の混合流について、数値計算と試験データの比較例を報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | There are lots of the mixing flows on the hypersupersonic transport propulsion system. For instance, the mixing between the exhaust jet and the entrained flow in the mixer-ejector nozzle to reduce the noise level at the take off and the mixing between the ram air and the turbo air in the front mixing component operating for the dual mode of the the hypersupersonic transport propulsion system. In the research and the development of this system it is very useful for predicting the mixing characteristics to design components and improve the performance of this system. In this paper the comparison between the analysis results and the test results of above two kinds flows are reported. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000294012 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-30 |